The monograph for the first time considered the principle and modern method of research and development of inertial bearing of the object of vision in the basic antenna coordinate system. which are based on a scientifically based set of methods and technical solutions , determining the theoretical and practical basis of the feasibility of the scientific and technical direction for the creation of an inertial measuring system , which is the inertial meter of the parameters of the viewing vector, and on its basis integrated airborne homing aircraft of various applications. The method of the process of inertial bearing of the object of sight is presented , allowing to form an algorithm for the functioning of integrated airborne homing of aircraft as a situational control algorithm in the form of procedures for automatic situation recognition and decision-making on homing modes. The monograph is intended for specialists in the field of design of integrated systems of various applications, and can also serve as a guide for graduate students and senior students of universities , Students in the field of system analysis, Management and Processing of Information , as well as instrumentation and radio engineering specialties.